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    AbstractDrag and its coefficient can be calculated by means ofvirtual environmental simulation with the help of wind tunnel or through

    computer software. The use of computer software makes it possible to be

    in time and cost savings. Numerical methods for doing this can be the

    fluid flow by a two dimensional or three-dimensional model of the vehicle

    structure to be resolved. This paper has tried to use the ANSYS !" and

    the e#uations governing fluid flow combined with standard model solved

    by using the appropriate boundary conditions. The study results of the

    aerodynamic analysis of the air flow$ pressure distribution and drag force

    on the vehicle. !ew design modifications in the form of attachable

    accessories have been suggested in order to reduce the drag coefficient.

    These modifications have shown a drag reduction of %&.'() at a speed of

    *+ km,h with the drag coefficient reduced to +.* from +.'$ therebyreducing the fuel consumption by about appro/imately %&.'()$ which

    means$ there is a saving of '.%&0 of petrol for every full tank refill. These

    observations are validated using wind tunnel testing on a %1'2 scaled

    model using momentum deficit method.

    3eywords: Automotive Aerodynamics4 Drag oefficient4 !uelonsumption4 Numerical Analysis4 Drag pressure4 5ind Tunnel

    Techni#ues$ 6omentum Deficit 6ethod$ !orce 7alance 6ethod

    INTRODUCTION

    Tata Nano was envisioned in 2003 to become a peoplesca! t"at is a##odable b$ eve$bod$! mainl$ t"e cit$ dwelleso# India% &ince its deb't in 200(! t"e sales o# Tata Nano "ave)one down temendo'sl$% In t"e #ist *'ate o# 20+3! n'mbe

    o# ve"icles sold in t"e mont"s o# ,an'a$! -eb'a$ and .ac"

    wee +/0! +/0/ and +/01 'nits! espectivel$% "en it was

    #ist conceived! a ta)et pice o# +00!000 'pees was

    establis"ed b't it cept 'p to abo't +2!000 'pees in ve$

    s"ot time d'e to a steep incease in pice o# aw mateials and

    inp't costs% dded to t"is! t"e soain) #'el pices! its no

    lon)e an easil$ a##odable ca% &t'dies "ave s"own t"at +/

    pecenta)e o# t"e #'el in a ve"icle is 'sed to ovecome

    mec"anical #iction in t"e en)ine! / pecenta)e o# t"e #'el is'sed to ovecome t"e ollin) esistance and da) is esponsible

    #o t"e emainin) 0pecenta)e% ca wit" low da) #oce

    enco'ntes lesse #iction t"an a ca wit" "i)"e da) #oce%

    4ence! a smalle en)ine is e*'ied to dive s'c" a ca w"ic"

    event'all$ lowes t"e #'el cons'mption% In t"is pape we

    #oc'ssed on ed'cin) t"e oveall da) #oce on t"e ve"icle! and

    5+ 6 sst% 7o#! Dept% o# eona'tical and 'tomobile 8n)) .ail:mani9andan%mmanipal%ed'!! 2!3! 6 &t'dents! .anipal Instit'te o#

    Tec"nolo)$! .anipal Univesit$! ;anata9aect

    ssociate! Indian Instit'te o# Tec"nolo)$! ?and"i Na)a! India%

    t"eeb$ bin)in) down t"e #'el cons'mption! "ence ma9in)t"e Tata Nano a)ain a #avo'ite amon) t"e Indian masses%

    @IT8RTUR8 R8AI8

    B'

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    obtained #o eac" velocit$% T"eoetical val'es wee validated

    b$ wind t'nnel test 'sin) pess'e tappin)s and pitot t'bes on

    a +:+/ model o# t"e ve"icle%

    ni9et ;'l9ani! & A &atis" and A &aavanan 829 nal$sed

    t"e #low patten o# a convetible #o two desi)ns i%e% wit" oo#

    closed and wit" oo# open% &edan models wee ceated 'sin)'todes9 Invento so#twae! mes" )eneation was done 'sin)

    ?ambit and #inall$ pocessed in -l'ent 'sin) 9

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    I.7ROAI&TION

    T"e vaio's desi)n modi#ications t"at wee anal$Fed ae as

    below

    i dam

    n ai dam ed'ces t"e aiect'e dawn was t"at t"e ma>oit$ o#

    t"e da) #oce on t"e ve"icle wo'ld be d'e to t"e wa9e e)ionbe"ind t"e ca and not mainl$ d'e to #ontal ai impact%

    Rea spoile

    Da) is ai p's"in) a)ainst t"e ve"icle as it moves% T"e #aste

    t"e ve"icle moves! t"e moe da)! w"ic" e*'ies moe powe

    and #'el to maintain t"e speed% spoiles p'pose is to

    ed'ce da)% n$ added s'#ace in ai#low adds to t"e da)%4oweve! )ood spoile desi)ns can ed'ce t"e oveall da) o#

    $o' ve"icle%

    4ence! t"e p'pose o# an a'tomotive spoile is to dis'pt! o

    spoil! t"e ai#low ove t"e ca to impove pe#omance% T"is

    desi)n ed'ced t"e da) #oce to +%322N

    Rea pot'sion

    ea pot'sion was desi)ned as s"own in t"e #i)'e PQQQ

    Rea sceen

    T"e best desi)n modi#ication came in t"e #om o# a ea

    sceen% T"e sceen was /mm in t"ic9ness and di##eent

    distances #om t"e ca ea wee anal$Fed%

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    T"e epected e##ect o# aeod$namic da) ed'cin) is ac"ieved

    #o t"e sa9e o# vote t"at oi)inates between ve"icle models

    ea wall and sceen t"e vote enables noectives and Investi)ationsX! w"ite pape!s'bmitted to NRC Decadal &'ve$ Inne 7lanets &'bpanel! ')'st20++%

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    P ColoFFa! %,%! Wis"ips #o 7laneta$ 8ploation,N&KCR